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Volume 38 Issue 8
Aug.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(8): 1124-1128.
Zhang Lijun, Cheng Peng. μ-Analysis and DFP Optimization Method of μ-Synthesis for Flight Control System[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 138-141. (in Chinese)
Citation: Hou Yunyi, Jing Qianfeng, Ma Guangfuet al. Orbital rendezvous control method for berthing and tracking approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1124-1128. (in Chinese)
shu

Orbital rendezvous control method for berthing and tracking approach

  • 1.

    School of Astronautics, Harbin Institute of Technology, Harbin 150001, China

  • 2. Shanghai Aerospace System Engineering Institute, Shanghai 201108, China

  • Received Date: 06 Jan 2011
  • Publish Date: 30 Aug 2012
    Abstract
  • The spacecraft orbital rendezvous technology is required for many missions, and the requirements of orbital control vary with the different tasks. In some cases, the tracker will be asked to stop in specified position temporarily; in other cases, the line-of-sight angle and trajectory are limited in the process of orbital rendezvous. To meet the different needs of various tasks, a closed-loop feedback control law was designed. By using this method of orbital control, the tracker can stop and keep in fixed point and approach target along the predetermined trajectory. The simulation shows that the control method has the advantages of fast tracking speed, high-accuracy, and low power consumption.

     

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    • References(6)
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